General Electric Company

Robert R Reed

Rahul Jaikaran Chillar

Douglas Scott Byrd

Julio Enrique Mestroni

Charles E Steber

The present application provides a liquid fuel system for use with a flow of a liquid fuel and a combustor of a gas turbine engine. The liquid fuel system may include a number of fuel lines in communication with the combustor, a purge air inlet positioned about each of the fuel lines, a number of drain lines with each drain line in communication with a respective fuel line, and a number of drain valves with each drain valve in communication with a respective drain line so as to drain the flow of liquid fuel in the fuel lines via a flow of purge air through the purge air inlet and opening the drain valves.

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Atlanta, GA, United States of America

Robert R Reed